Casualties unknown

Engine Failure and Hard Landing Following Cylinder Head Fatigue Fracture (N15367)

Homedale, ID, US

On September 3, 2003, a Piper PA-28-140 (registration N15367) was involved in an aviation accident near Homedale, ID. Investigators recorded the probable cause as: The cylinder head fractured due to fatigue. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

An airplane experienced engine vibration and subsequent power loss, leading to a hard landing that collapsed the pilot's seat. Examination revealed a fatigue fracture in the number four cylinder head.

Event Description

During cruise flight, the pilot noticed an uncharacteristic vibration from the engine. Diverting to a nearby airport, the pilot entered a downwind leg for the intended runway when the engine stopped producing power. The pilot then turned directly toward runway 31. After completing the turn to final approach, the pilot landed on the intended runway, describing the touchdown as "very hard." Following the landing, the pilot's seat was found to have collapsed as a result of the impact.

Engine Examination

Inspection of the aircraft's engine revealed a fracture in the number four cylinder head. The fracture extended entirely through the cylinder head, originating from the top sparkplug hole and running around the circumference to the bottom sparkplug hole. A metallurgical examination determined that the cylinder head failed due to fatigue. Multiple fatigue crack initiation sites were identified, most notably a series of cracks that began at each of the two sparkplug holes.

Maintenance History

Maintenance records indicated that the failed cylinder had been previously repaired for valve pitting and returned to service. At the time of the repair, the engine had accumulated 6,689 total hours and 726 hours since a major overhaul. The total time since manufacture for the cylinder itself could not be determined. At the time of the accident, the engine total time was approximately 7,260 hours, with 1,319 hours since the last major overhaul.

Conclusion

The metallurgical examination concluded that the cylinder head fractured due to fatigue, with multiple initiation sites at the sparkplug holes.

Probable cause

The cylinder head fractured due to fatigue.

Frequently asked questions

What happened in the 3 Sept 2003 Piper PA-28-140 accident near Homedale, ID?

An airplane experienced engine vibration and subsequent power loss, leading to a hard landing that collapsed the pilot's seat. Examination revealed a fatigue fracture in the number four cylinder head.

What aircraft was involved and where did it happen?

The accident on 3 Sept 2003 involved a Piper PA-28-140, registration N15367, at Homedale, ID.

What was the probable cause of the accident?

The cylinder head fractured due to fatigue.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030910X01512. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.